Piezoelectric Actuators Used for Helicopter Vibration Reduction

Zhu Zhang; Wei Dong Yang; Da Lin Yang

doi:10.4028/www.scientific.net/AMR.718-720.1729

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 718-720Piezoelectric Actuators Used for Helicopter...

Piezoelectric Actuators Used for Helicopter Vibration Reduction

Abstract:

This paper covers the development of two piezoelectric actuators for trailing edge flap control on mach scaled model helicopter rotors. The design, analysis and bench tests of these two actuators are described. Under different voltages and frequencies, their drive performances are tested and compared. Results showed that these two actuators all can effectively drive and control the flaps with each advantages and disadvantages.

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Periodical:

Advanced Materials Research (Volumes 718-720)

Pages:

1729-1733

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.718-720.1729

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Online since:

July 2013

Authors:

Zhu Zhang, Wei Dong Yang, Da Lin Yang

Keywords:

Helicopter Vibration Reduction, Piezoelectric Actuator, Piezoelectric Ceramic (PZT), Smart Rotor, Trailing Edge Flap

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References

[1] Enenkl B, Kloppel V, et al. Full Scale Rotor with Piezoelectric Actuated Blade Flaps, Proc.28th European Rotorcraft Forum. Bristol: 2002: Paper 89.

Google Scholar

[2] Koratkar, N.A, Chopra, I. Wind Tunnel Testing of a Mach-Scaled Rotor Model with Trailing Edge Flaps, Proc. 57th AHS Annual Forum. Alexandria: 2001: 1069-1099.

DOI: 10.2514/6.2001-1358

Google Scholar

[3] Peter Konstanzer, Bernhard Enenkl, et al. Recent advances in Eurocopter's passive and active vibration control, American Helicopter Society 64th Annual Forum. Canada: 2008.

Google Scholar

[4] Straub, F.K. et al. Development and whirl tower testing of the SMART active flap rotor, Proc. SPIE Symposium on Smart Structures and Materials. San Diego: 2004.

DOI: 10.1117/12.562645

Google Scholar

[5] F. Straub, V. Anand, D. Domzalski. Development of a Piezoelectric Actuator for Trailing Edge Flap Control of Full Scale Rotor Blades, Smart Materials and Structures, 2001.

DOI: 10.1088/0964-1726/10/1/303

Google Scholar

[6] Zhang Zhu, Design, Analysis and Test of Smart Rotor Based on the High Effective Actuator, Nanjing University of Aeronautics and Astronautics, Nanjing, China.

Google Scholar